Piper PA-28-161 Maintenance Manual

PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 6
Nov 30/06
3D22
32-10-00
C. Installation (Refer to Figure 2.)
(1) The main landing gear assembly may be installed on the wing by the following procedure:
(a) Position the gear up in the wing through the access opening and secure with bolts,
washers and nuts.
(b) Reconnect the brake line at the point of disconnection.
(2) Service the oleo strut per Oleo Struts, 12-10-00.
(3) Service the brake system. (Refer to Brake System, 12-10-00.)
(4) Install the access plate to the bottom of the wing and the oleo housing fairing to the rear.
(5) Slide the drip pan from under the gear and remove the airplane from the jacks.

Piper PA-28-161 Specifications

General

Manufacturer	Piper Aircraft
Model	PA-28-161 Warrior II
Engine	Lycoming O-320-D3G
Horsepower	160 hp
Seating Capacity	4
Wingspan	35 ft (10.7 m)
Length	24 ft 0 in
Maximum Speed	127 knots
Cruise Speed	122 knots
Maximum Takeoff Weight	2, 325 lb (1, 055 kg)
Fuel Capacity	48 US gallons (182 L)